| 摘要 |
The present invention relates to a mold for a C-shaped spar of an aircraft. The mold for a C-shaped spar of an aircraft comprises: a mold body wherein a composite material is wound on an outer surface thereof to form a C-shaped spar; a bracket mounted on both ends of the mold body; and a binding unit wherein one side thereof is mounted on both ends of the bracket and the other side thereof is mounted on a drive shaft rotated by a rotating means to rotate the mold body. The mold body comprises: an external structure whose both sides are opened, and which has an empty space therein, and is formed in a rectangular shape to wind the composite material on the outside thereof; an internal structure installed in the external structure and formed in a grid shape to reinforce strength and allow air to flow to both sides thereof; a side panel installed on both ends of the external structure and provided with a plurality of air outflow holes to allow air to flow thereinto and discharge air therefrom; and a connection structure installed on the side panel and formed in a disk connected to the bracket. |
